This is an engine power performance test equipment on the ground in the early stages for the research and development of UAV (MUAV). In the propeller mounted condition, it consists of engine thrust measurement Bed considering the air flow, fuel supply device, a scavenger oil cooling device, electrical backup devices, an intercom equipment, equipment integration controls, an engine monitoring equipment, a test data acquisition system, and a connection interface duct for existing aircraft environmental test chamber and we successfully have delivered it.


PT6A-67 Engine performance ground-test facility